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Tachikawa Ki-36

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Japanese army cooperation aircraft
Ki-36
General information
TypeTwo-seat Army Co-operation Aircraft
ManufacturerTachikawa Aircraft Company Ltd
Primary usersImperial Japanese Army Air Force Royal Thai Air Force
Number built1,334
History
Manufactured1938 - 1944
First flight20 April 1938
VariantsTachikawa Ki-55

The Tachikawa Ki-36 (named Ida in Allied reporting code) was a Japanese army co-operation aircraft of World War II. It was a two-seat, low-wing monoplane with a single piston engine and fixed, tailwheel-type undercarriage.

Design and development

The prototype, fitted with a 450 hp (336 kW) Hitachi Army Type 98 Ha-13 engine, first flew on 20 April 1938. Having outperformed the Mitsubishi Ki-35 in comparative trials, the Ki-36 was designated the Army Type 98 Direct Co-operation Aircraft and ordered into production in November 1938. Production ended in January 1944 after a total of 1,334 Ki-36 had been built (Tachikawa 862 and Kawasaki 472).

Operational history

The Ki-36 first saw action in China where it saw success. Later, in the Pacific, it proved excessively vulnerable to opposing fighters. It was thereafter redeployed to the safer theater of China. Towards the end of the war, the Ki-36 was employed as a kamikaze aircraft with a bomb of 500-kg (1,102-lb) fitted externally.

Variants

  • Ki-55: Two-seat advanced trainer version.
  • Ki-72: An evolved version with a 600-hp (447-kW) Hitachi Ha-38 engine and retractable undercarriage. Not built.

Operators

Tachikawa Ki-36 trainer at the Royal Thai Air Force Museum.
 People's Republic of China
 Indonesia
 Japan
 Thailand

Specifications (Ki-36)

Data from Japanese Aircraft of the Pacific War, and The Concise Guide to Axis Aircraft of World War II

General characteristics

  • Crew: 2
  • Length: 8 m (26 ft 3 in)
  • Wingspan: 11.8 m (38 ft 9 in)
  • Height: 3.64 m (11 ft 11 in)
  • Wing area: 20 m (220 sq ft)
  • Airfoil: root: NACA 23014; tip: NACA 23006
  • Empty weight: 1,247 kg (2,749 lb)
  • Gross weight: 1,660 kg (3,660 lb)
  • Powerplant: 1 × Hitachi Ha13a (Army Type 98 450hp Air Cooled Radial) 9-cylinder air-cooled radial piston engine, 380 kW (510 hp) for take-off
350 kW (470 hp) at 1,700 m (5,600 ft)

Performance

  • Maximum speed: 348 km/h (216 mph, 188 kn)
  • Cruise speed: 235 km/h (146 mph, 127 kn)
  • Range: 1,235 km (767 mi, 667 nmi)
  • Service ceiling: 8,150 m (26,740 ft)
  • Time to altitude: 3,000 m (9,800 ft) in 6 minutes 39 seconds
  • Wing loading: 83 kg/m (17 lb/sq ft)
  • Power/mass: 0.23 kW/kg (0.14 hp/lb)

Armament

  • Guns: one fixed, forward-firing 7.7 mm (0.303 in) Type 89 machine gun, one flexible 7.7 mm (0.303 in) Type 89 machine gun in the rear cockpit.
  • Bombs: up to 350 kg (772 lb) external bombload

See also

Related development

Related lists

References

Citations

  1. Francillon 1979, p. 254.
  2. ^ Francillon 1979, p. 253.
  3. Mondey 1996, p. 246.
  4. Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.

Bibliography

External links

Tachikawa aircraft
Imperial Japanese Army types
World War II Allied reporting names
Imperial Japanese Army Air Service aircraft designations
1-50
51-100
100-
World War II Allied reporting names for Japanese aircraft
Aircraft in Japanese service
Foreign aircraft
thought to be in Japanese service
  • Bess (Heinkel He 111)
  • Doc (Messerschmitt Bf 110)
  • Fred (Focke Wulf Fw 190)
  • Irene (Junkers Ju 87)
  • Janice (Junkers Ju 88)
  • Mike (Messerschmitt Bf 109)
  • Millie (Vultee V-11)
  • Trixie (Junkers Ju 52)
  • Trudy (Focke-Wulf Fw 200)
Royal Thai Armed Forces trainer aircraft designations
B.F
(Trainer)
B.KhF
(Fighter-trainer)
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